TERMIUM Plus^®

Record 1,  Textual support,  English

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 DEF

Partie la plus en retrait de la zone portuaire située après le franchissement de l'écluse qui le sépare de l'avant-port.  2, record 1, French, - arri%C3%A8re%2Dport

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

The rudder actuator is a tandem actuator, having two internal piston areas for each hydraulic source(A & B). The actuator is capable of positioning the rudder panel with either one or both main hydraulic sources available, though with one source inoperative a reduced rudder panel deflection would result due to blowdown at higher airspeeds. Flow of hydraulic fluid to the rudder actuator is controlled by the dual servo-valve. This is a complex dual concentric cylinder with an outer and inner slide. During normal rudder pedal inputs sufficient rudder panel deflection is catered for by the primary(inner) valve alone. However, should a larger panel deflection be required or a higher rate rudder input be commanded, the secondary(outer) sleeve moves in addition to port extra fluid to the actuator. Movement of the outer sleeve is typically no more than 1 mm. Position of both sleeves of the servo valve is controlled by a complex mechanism of bell cranks, input rod and summing lever, the geometry of which is such as to provide movement of the sleeves in relation to the body of the valve.  2, record 2, English, - rudder%20actuator

Record number: 2, Textual support number: 1 OBS

Equivalent found on a cutaway diagram of a Boeing 767.  3, record 2, English, - rudder%20actuator

Record number: 2, Textual support number: 2 OBS

rudder actuator: term standardized by ISO.  4, record 2, English, - rudder%20actuator

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

servocommande de direction : terme normalisé par l'ISO; vérin de direction: terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  4, record 2, French, - servocommande%20de%20direction

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

Both gear-and gerotor-type pumps are used in the lubricating system of the turbine engine.... The Gerotor pump has two moving parts : an inner-toothed element meshing with an outer-toothed element. The inner element has one less tooth than the outer. The missing tooth provides a chamber to move the fluid from the intake to the discharge port. Both elements are mounted eccentrically to one another on the same shaft.  3, record 3, English, - gerotor%2Dtype%20pump

Record number: 3, Textual support number: 2 CONT

Pitot pumps are seldom used in gearbox lubrication systems, as it is more common to employ a positive displacement pump such as a gear pump or a gerotor type pump.  2, record 3, English, - gerotor%2Dtype%20pump

Record number: 3, Textual support number: 1 OBS

gerotor: A gear-within-gear pump that consists of an inner gear with one less tooth than the outer gear.  4, record 3, English, - gerotor%2Dtype%20pump

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

Les pompes à engrenages utilisent le profil combiné de deux roues dentées pour transvaser et augmenter la pression d'un fluide. Elles sont exclusivement utilisées avec des liquides.  2, record 3, French, - pompe%20%C3%A0%20engrenages%20embo%C3%AEt%C3%A9s

Record number: 3, Textual support number: 2 OBS

pompe à engrenages emboîtés : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  3, record 3, French, - pompe%20%C3%A0%20engrenages%20embo%C3%AEt%C3%A9s

Record 3,  Textual support,  Spanish